Amirkabir University of Technology Amirkabir Journal of Mechanical Engineering 2008-6032 52 10 2019 09 28 Experimental Investigation on the Inter-Laminar Strength in a Hybrid Elastomer Modified Fiber Metal Laminate Under High and Low-Velocity Impact and QuasiStatic Bendin Experimental Investigation on the Inter-Laminar Strength in a Hybrid Elastomer Modified Fiber Metal Laminate Under High and Low-Velocity Impact and QuasiStatic Bendin 2931 2950 3602 10.22060/mej.2019.16385.6358 FA Mohammad Amin Zarezadeh Mehrizi Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran Alireza Taherzadeh-Fard Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran Gholamhossein Liaghat Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran Hamed Ahmadi Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran Yavar Anani Post. Doc. Researcher,Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran Amin Khodadadi Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran S.Samaneh Asemani Department of Mechanical Engineering, Tarbiat Modares University, Tehran, Iran Journal Article 2019 05 22 Growing the need to impact resistive structures, hybrid laminates have been absorbed much attention. To reach appropriate strength, high stiffness, and good energy absorption, the interfacial adhesion between different layers is important. The present paper is an attempt to assess the adhesion between different layers in a hybrid laminate consists of natural rubber, glass/epoxy composite and two layers of aluminum under high and low-velocity impact and quasi-static three-point bending conditions. In order to minimize the debonding, three kinds of specimens were made by three different adhesives including Chemosil 222 and its primer, Bylamet S2 and Cyanoacrylate. Based on the results obtained from high and low-velocity impact tests, the best choice for elastomer/composite, composite/aluminum and elastomer/aluminum interfaces are bylamet S2, cyanoacrylate, and chemosil, respectively according to delaminated area. Samples containing bylamet S2 adhesive in all interfaces have a better performance in terms of dynamic stiffness. Growing the need to impact resistive structures, hybrid laminates have been absorbed much attention. To reach appropriate strength, high stiffness, and good energy absorption, the interfacial adhesion between different layers is important. The present paper is an attempt to assess the adhesion between different layers in a hybrid laminate consists of natural rubber, glass/epoxy composite and two layers of aluminum under high and low-velocity impact and quasi-static three-point bending conditions. In order to minimize the debonding, three kinds of specimens were made by three different adhesives including Chemosil 222 and its primer, Bylamet S2 and Cyanoacrylate. Based on the results obtained from high and low-velocity impact tests, the best choice for elastomer/composite, composite/aluminum and elastomer/aluminum interfaces are bylamet S2, cyanoacrylate, and chemosil, respectively according to delaminated area. Samples containing bylamet S2 adhesive in all interfaces have a better performance in terms of dynamic stiffness. https://mej.aut.ac.ir/article_3602_228b25587479f2fc7570428e8bcbabdc.pdf